METHOD AND DEVICE FOR DETERMINING AERODYNAMIC CHARACTERISTICS OF AN AIRCRAFT
First Claim
1. A method for determining aerodynamic characteristics of an aircraft comprising the steps:
- (a) Detecting forces and mechanical flight parameters on aerofoils and a horizontal tail plane of the aircraft at various detection instants during at least one non-stationary flight manoeuvre of the aircraft; and
(b) Evaluation of a system of equations, which comprises, for each detection instant, a pitch movement moment balance equation, which has the detected forces and mechanical flight parameters, to calculate the aerodynamic characteristics of the aircraft.
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Abstract
The present invention provides a device and method for determining aerodynamic characteristics of an aircraft, in particular a pitch moment coefficient at an ascending force of the aircraft without a horizontal tail plane of zero and an aerodynamic neutral point of the aircraft without a horizontal tail plane. In the method according to the invention, forces and mechanical flight parameters on aerofoils and a horizontal tail plane of the aircraft are detected at various detection instants during at least one non-stationary flight manoeuvre of the aircraft. In this case, a linear system of equations is formed, which comprises a pitch movement moment balance equation for each detection instant, the pitch movement moment balance equation having the detected forces and mechanical flight parameters. This linear system of equations is evaluated to calculate the aerodynamic characteristics.
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Citations
15 Claims
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1. A method for determining aerodynamic characteristics of an aircraft comprising the steps:
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(a) Detecting forces and mechanical flight parameters on aerofoils and a horizontal tail plane of the aircraft at various detection instants during at least one non-stationary flight manoeuvre of the aircraft; and (b) Evaluation of a system of equations, which comprises, for each detection instant, a pitch movement moment balance equation, which has the detected forces and mechanical flight parameters, to calculate the aerodynamic characteristics of the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 14, 15)
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11. A device for determining aerodynamic characteristics of an aircraft comprising:
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(a) Sensors for detecting forces and mechanical flight parameters on aerofoils and a horizontal tail plane of the aircraft at various detection instants during at least one non-stationary flight manoeuvre of the aircraft; and
comprising(b) A calculation unit to evaluate a system of equations, which for each detection instant comprises a pitch movement moment balance equation, which has the detected forces and mechanical flight parameters to calculate the aerodynamic characteristics of the aircraft. - View Dependent Claims (12, 13)
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Specification